The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 09, 2020

Filed:

Aug. 19, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Daniel Alan Niergarth, Cincinnati, OH (US);

Randy M. Vondrell, Cincinnati, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Patrick Michael Marrinan, Mason, OH (US);

Lawrence Chih-hui Cheung, Niskayuna, NY (US);

Nikolai N. Pastouchenko, Glenville, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/08 (2006.01); F02K 5/00 (2006.01); F02C 7/14 (2006.01); F02C 6/20 (2006.01); B64C 11/00 (2006.01); B64C 21/06 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F02K 3/062 (2006.01); F04D 29/056 (2006.01); F04D 29/063 (2006.01); F04D 29/32 (2006.01); F04D 29/58 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 33/08 (2013.01); B64C 11/001 (2013.01); B64C 21/06 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F02C 6/206 (2013.01); F02C 7/14 (2013.01); F02K 3/062 (2013.01); F02K 5/00 (2013.01); F04D 29/056 (2013.01); F04D 29/063 (2013.01); F04D 29/325 (2013.01); F04D 29/582 (2013.01); B64D 2027/026 (2013.01); F05D 2220/323 (2013.01); F05D 2260/213 (2013.01); F05D 2260/98 (2013.01); Y02T 50/676 (2013.01);
Abstract

A propulsion system for an aircraft includes an electric propulsion engine. The electric propulsion engine includes an electric motor and a fan rotatable about a central axis of the electric propulsion engine by the electric motor. The electric propulsion engine also includes a bearing supporting rotation of the fan and a thermal management system. The thermal management system includes a lubrication oil circulation assembly and a heat exchanger thermally connected to the lubrication oil circulation assembly. The lubrication oil circulation assembly is configured for providing the bearing with lubrication oil. Such an electric propulsion engine may be a relatively self-sufficient engine.


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